What was found
WHILE ATTEMPTING TO INSTALL TIP CAP ONTO MAIN ROTOR BLADE, DISCOVERED INSUFFICIENT CLEARANCE BETWEEN INNER DOUBLERS - WILL NOT FIT FORWARD END OF TIP PLATE. COMPONENT P/N 76150-09100-952.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE ATTEMPTING TO INSTALL TIP CAP ONTO MAIN ROTOR BLADE, DISCOVERED INSUFFICIENT CLEARANCE BETWEEN INNER DOUBLERS - WILL NOT FIT FORWARD END OF TIP PLATE. COMPONENT P/N 76150-09100-952.